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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.3 at α=2.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs03182-il-1000000-n5.txt
Download as CSV file: xf-fxs03182-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.4215   0.12934   0.12741  -0.0694   0.9464   0.0019
 -16.250  -0.4818   0.11011   0.10803  -0.0772   0.9457   0.0018
 -16.000  -0.5181   0.09452   0.09223  -0.0867   0.9409   0.0018
 -15.750  -0.5312   0.08229   0.07979  -0.0977   0.9339   0.0017
 -15.500  -0.5405   0.07110   0.06834  -0.1095   0.9258   0.0017
 -15.250  -0.5417   0.06132   0.05821  -0.1217   0.9080   0.0017
 -15.000  -0.5455   0.05516   0.05172  -0.1279   0.8801   0.0017
 -14.750  -0.5515   0.05121   0.04751  -0.1298   0.8548   0.0017
 -14.500  -0.5548   0.04814   0.04425  -0.1308   0.8366   0.0017
 -14.250  -0.5592   0.04515   0.04108  -0.1313   0.8218   0.0017
 -14.000  -0.5648   0.04223   0.03797  -0.1315   0.8084   0.0017
 -13.500  -0.5683   0.03749   0.03290  -0.1311   0.7864   0.0017
 -13.250  -0.5678   0.03550   0.03075  -0.1306   0.7774   0.0017
 -13.000  -0.5646   0.03377   0.02889  -0.1300   0.7691   0.0017
 -12.750  -0.5627   0.03194   0.02691  -0.1292   0.7618   0.0017
 -12.500  -0.5576   0.03042   0.02526  -0.1284   0.7543   0.0017
 -12.250  -0.5542   0.02875   0.02345  -0.1272   0.7479   0.0018
 -12.000  -0.5432   0.02778   0.02238  -0.1266   0.7413   0.0017
 -11.750  -0.5355   0.02651   0.02099  -0.1256   0.7355   0.0017
 -11.500  -0.5256   0.02542   0.01981  -0.1246   0.7295   0.0017
 -11.000  -0.5047   0.02340   0.01760  -0.1225   0.7186   0.0018
 -10.750  -0.4937   0.02244   0.01655  -0.1213   0.7131   0.0018
 -10.500  -0.4828   0.02152   0.01555  -0.1200   0.7082   0.0018
 -10.250  -0.4697   0.02073   0.01469  -0.1190   0.7036   0.0018
 -10.000  -0.4581   0.01988   0.01376  -0.1177   0.6989   0.0018
  -9.750  -0.4452   0.01916   0.01297  -0.1164   0.6948   0.0018
  -9.500  -0.4313   0.01846   0.01222  -0.1153   0.6912   0.0018
  -9.250  -0.4188   0.01772   0.01141  -0.1139   0.6874   0.0019
  -9.000  -0.4042   0.01714   0.01078  -0.1127   0.6837   0.0019
  -8.500  -0.3781   0.01588   0.00942  -0.1097   0.6775   0.0019
  -8.250  -0.3655   0.01529   0.00879  -0.1080   0.6744   0.0019
  -8.000  -0.3544   0.01481   0.00827  -0.1060   0.6713   0.0020
  -7.750  -0.3457   0.01427   0.00768  -0.1036   0.6683   0.0020
  -7.500  -0.3324   0.01366   0.00699  -0.1020   0.6655   0.0022
  -7.250  -0.3129   0.01327   0.00656  -0.1012   0.6631   0.0022
  -7.000  -0.2922   0.01291   0.00616  -0.1006   0.6603   0.0023
  -6.750  -0.2708   0.01256   0.00578  -0.1000   0.6576   0.0026
  -6.500  -0.2479   0.01228   0.00546  -0.0996   0.6550   0.0026
  -6.250  -0.2247   0.01200   0.00514  -0.0993   0.6527   0.0030
  -6.000  -0.2004   0.01174   0.00484  -0.0992   0.6507   0.0031
  -5.750  -0.1751   0.01151   0.00458  -0.0991   0.6487   0.0035
  -5.500  -0.1494   0.01129   0.00434  -0.0992   0.6467   0.0036
  -5.250  -0.1239   0.01104   0.00406  -0.0992   0.6446   0.0041
  -5.000  -0.0978   0.01082   0.00381  -0.0993   0.6426   0.0047
  -4.750  -0.0714   0.01062   0.00358  -0.0995   0.6407   0.0064
  -4.500  -0.0449   0.01043   0.00341  -0.0997   0.6388   0.0144
  -4.250  -0.0176   0.01032   0.00329  -0.0999   0.6371   0.0159
  -4.000   0.0100   0.01015   0.00313  -0.1003   0.6356   0.0183
  -3.750   0.0379   0.01001   0.00299  -0.1007   0.6341   0.0199
  -3.500   0.0660   0.00990   0.00287  -0.1011   0.6324   0.0206
  -3.250   0.0941   0.00979   0.00276  -0.1015   0.6306   0.0236
  -3.000   0.1220   0.00962   0.00264  -0.1019   0.6288   0.0362
  -2.750   0.1503   0.00953   0.00254  -0.1023   0.6272   0.0429
  -2.500   0.1784   0.00938   0.00244  -0.1028   0.6257   0.0605
  -2.250   0.2065   0.00915   0.00232  -0.1034   0.6243   0.0989
  -1.750   0.2663   0.00699   0.00158  -0.1073   0.6218   0.5232
  -1.500   0.2962   0.00697   0.00160  -0.1080   0.6206   0.5471
  -1.250   0.3259   0.00697   0.00163  -0.1086   0.6194   0.5586
  -1.000   0.3555   0.00699   0.00164  -0.1092   0.6181   0.5662
  -0.750   0.3850   0.00700   0.00167  -0.1098   0.6168   0.5735
  -0.500   0.4145   0.00704   0.00170  -0.1104   0.6153   0.5817
  -0.250   0.4437   0.00708   0.00175  -0.1109   0.6129   0.5903
   0.000   0.4723   0.00715   0.00178  -0.1112   0.6093   0.5950
   0.250   0.5013   0.00714   0.00178  -0.1117   0.6042   0.5963
   0.500   0.5302   0.00716   0.00181  -0.1122   0.6004   0.5985
   0.750   0.5590   0.00721   0.00185  -0.1126   0.5972   0.6020
   1.000   0.5875   0.00728   0.00190  -0.1129   0.5943   0.6056
   1.250   0.6167   0.00730   0.00193  -0.1134   0.5910   0.6079
   1.750   0.6720   0.00738   0.00196  -0.1139   0.5695   0.6100
   2.000   0.6997   0.00744   0.00200  -0.1141   0.5601   0.6113
   2.250   0.7261   0.00754   0.00206  -0.1140   0.5431   0.6126
   2.500   0.7471   0.00787   0.00219  -0.1130   0.4977   0.6138
   2.750   0.7322   0.00993   0.00328  -0.1056   0.3031   0.6150
   3.000   0.7327   0.01108   0.00396  -0.1010   0.1983   0.6162
   3.250   0.7344   0.01193   0.00448  -0.0965   0.1248   0.6175
   3.500   0.7429   0.01248   0.00487  -0.0933   0.0847   0.6187
   3.750   0.7553   0.01299   0.00527  -0.0908   0.0536   0.6200
   4.000   0.7737   0.01332   0.00556  -0.0894   0.0454   0.6212
   4.250   0.7905   0.01371   0.00590  -0.0879   0.0336   0.6223
   4.750   0.8284   0.01434   0.00654  -0.0856   0.0272   0.6250
   5.000   0.8469   0.01468   0.00690  -0.0844   0.0236   0.6266
   5.250   0.8611   0.01522   0.00742  -0.0826   0.0134   0.6282
   5.500   0.8781   0.01567   0.00787  -0.0813   0.0122   0.6297
   5.750   0.8949   0.01614   0.00835  -0.0800   0.0104   0.6312
   6.000   0.9123   0.01661   0.00884  -0.0789   0.0096   0.6328
   6.250   0.9297   0.01709   0.00934  -0.0778   0.0092   0.6344
   6.500   0.9468   0.01761   0.00988  -0.0768   0.0082   0.6359
   6.750   0.9628   0.01821   0.01049  -0.0756   0.0061   0.6374
   7.000   0.9763   0.01896   0.01125  -0.0741   0.0021   0.6389
   7.250   0.9924   0.01960   0.01192  -0.0731   0.0019   0.6407
   7.500   1.0079   0.02029   0.01265  -0.0720   0.0018   0.6426
   7.750   1.0229   0.02103   0.01343  -0.0709   0.0017   0.6447
   8.000   1.0378   0.02180   0.01424  -0.0698   0.0016   0.6470
   8.250   1.0526   0.02260   0.01508  -0.0688   0.0016   0.6491
   8.500   1.0667   0.02346   0.01598  -0.0677   0.0015   0.6512
   9.000   1.0944   0.02527   0.01787  -0.0657   0.0014   0.6552
   9.250   1.1076   0.02625   0.01891  -0.0646   0.0014   0.6576
   9.500   1.1194   0.02735   0.02007  -0.0635   0.0013   0.6600
   9.750   1.1318   0.02841   0.02118  -0.0625   0.0012   0.6625
  10.000   1.1430   0.02960   0.02244  -0.0614   0.0011   0.6650
  10.250   1.1555   0.03072   0.02360  -0.0605   0.0011   0.6674
  10.500   1.1680   0.03186   0.02480  -0.0597   0.0011   0.6701
  10.750   1.1808   0.03298   0.02598  -0.0589   0.0011   0.6730
  11.000   1.1925   0.03423   0.02728  -0.0581   0.0011   0.6760
  11.250   1.2042   0.03551   0.02861  -0.0573   0.0011   0.6791
  11.500   1.2158   0.03682   0.02998  -0.0565   0.0010   0.6821
  11.750   1.2270   0.03818   0.03140  -0.0558   0.0010   0.6855
  12.000   1.2377   0.03962   0.03291  -0.0551   0.0010   0.6893
  12.250   1.2483   0.04109   0.03446  -0.0544   0.0010   0.6932
  12.500   1.2588   0.04260   0.03603  -0.0538   0.0009   0.6967
  12.750   1.2689   0.04418   0.03768  -0.0533   0.0009   0.7005
  13.000   1.2790   0.04578   0.03935  -0.0527   0.0009   0.7046
  13.250   1.2876   0.04756   0.04120  -0.0522   0.0009   0.7087
  13.500   1.2975   0.04924   0.04295  -0.0518   0.0009   0.7128
  13.750   1.3052   0.05120   0.04499  -0.0513   0.0008   0.7173
  14.000   1.3134   0.05313   0.04700  -0.0509   0.0008   0.7223
  14.500   1.3275   0.05733   0.05139  -0.0503   0.0008   0.7320
  14.750   1.3338   0.05959   0.05373  -0.0501   0.0008   0.7375
  15.000   1.3402   0.06188   0.05611  -0.0499   0.0007   0.7428
  15.250   1.3452   0.06438   0.05871  -0.0499   0.0007   0.7486
  15.500   1.3493   0.06704   0.06147  -0.0499   0.0007   0.7545
  15.750   1.3535   0.06973   0.06426  -0.0500   0.0007   0.7605
  16.000   1.3566   0.07263   0.06727  -0.0501   0.0007   0.7672
  16.250   1.3592   0.07566   0.07041  -0.0504   0.0006   0.7739
  16.500   1.3606   0.07891   0.07377  -0.0509   0.0006   0.7813
  16.750   1.3614   0.08231   0.07729  -0.0514   0.0006   0.7886
  17.000   1.3612   0.08591   0.08101  -0.0521   0.0006   0.7967
  17.250   1.3592   0.08989   0.08512  -0.0529   0.0006   0.8044
  17.500   1.3577   0.09386   0.08922  -0.0540   0.0006   0.8132
  17.750   1.3543   0.09823   0.09373  -0.0552   0.0006   0.8227
  18.000   1.3496   0.10287   0.09851  -0.0567   0.0005   0.8329
  18.250   1.3444   0.10768   0.10347  -0.0584   0.0005   0.8449
  18.500   1.3384   0.11272   0.10866  -0.0603   0.0005   0.8591
  18.750   1.3299   0.11817   0.11430  -0.0624   0.0005   0.8772
  19.000   1.3205   0.12336   0.11968  -0.0642   0.0005   0.9114
  19.250   1.3085   0.12817   0.12467  -0.0653   0.0005   1.0000
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